View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 55582U 26145.41497898 +.00000000 +00000-0 -36361-4 0 00000
2 55582 43.0032 280.9147 0001205 269.3993 90.6721 15.27582997 09
| Epoch (UTC): | 25 May 2026 09:57:34 |
| Eccentricity: | 0.0001205 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 280.9147° |
| argument of perigee: | 269.3993° |
| revolutions per day: | 15.27582997 |
| mean anomaly at epoch: | 90.6721° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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